FormFactorWing:

Path: ACPro/ACUtils

% Computes the form factor for a wing.

   The drag on a lifting surface is k cF S where S is the wetted
   area and cF is the skin friction coefficient.

   Type FormFactorWing for demo.

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   Form:
   k = FormFactorWing( m, t, lambda )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   m          (1,:)   Mach number
   t          (1,:)   Thickness ratio t/c
   lambda     (1,1)   Sweep angle

   -------
   Outputs
   -------
   k          (1,:)   Form factor

--------------------------------------------------------------------------
   Reference:  http://adg.stanford.edu/aa241/drag/lsformfactor.html
--------------------------------------------------------------------------

Children:

Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

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